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Flow Duct

Application ID: 1371

The modeling of aircraft-engine noise is a central problem in the field of computational aeroacoustics. The acoustic field in a model of an axially symmetric aero-engine duct, generated by a noise source at the boundary, is computed and visualized.

Results are presented for situations with as well as without a compressible irrotational background flow and for the cases of hard and lined duct walls.

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